Ground tests to minimize development risks and limit the number of development cycles

Saxena, SK and Ravi, K (1994) Ground tests to minimize development risks and limit the number of development cycles. In: 12th AIAA Applied Aerodynamics Conference, 20-22 June 1994, Colorado Springs.

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Abstract

13; Abstract Attention is given to ground tests designed for reduction of development and operational risks, and for participation in the qualification or certification of aircraft. Consideration is given to tests involved in the following three areas: the means employed, on the one hand, to reduce the risks to a minimum, and, on the other, to decrease the cycle, both in number of phases and duration, during development; ways in which performance data and schedules are produced for fatigue tests; and static tests on airframes of large aircraft. Recent examples in the military and civilian fields are reported. 13;

Item Type: Conference or Workshop Item (Paper)
Uncontrolled Keywords: Three dimrnsional flow;Supersonic flow;Inviscid flow
Subjects: AERONAUTICS > Aerodynamics
Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
Depositing User: M/S ICAST NAL
Date Deposited: 03 Oct 2006
Last Modified: 24 May 2010 09:50
URI: http://nal-ir.nal.res.in/id/eprint/2816

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